A single, unitary fuel/oil manifold for a gas turbine engine is provided which comprises one or more interfaces for mounting various fuel system and lubricating system components directly to the fuel/oil manifold. The fuel/oil manifold also defines fluid passages for transferring fuel or lubricant from one component to another component. Packing numerous fuel system and lubricating system components within the fuel/oil manifold reduces cost and weight and simplifies maintenance.
申请公布号
EP3008311(A4)
申请公布日期
2016.07.20
申请号
EP20140811004
申请日期
2014.02.27
申请人
UNITED TECHNOLOGIES CORPORATION
发明人
DREHER, MICHAEL;SNYDER, RYAN, K.;MCPHERSON, JAMES, M.;SU, PING;QUINONES, FERNANDO;RIVERA, GABRIEL